RU2522017C2 - Реверсор тяги - Google Patents
Реверсор тяги Download PDFInfo
- Publication number
- RU2522017C2 RU2522017C2 RU2011152808/06A RU2011152808A RU2522017C2 RU 2522017 C2 RU2522017 C2 RU 2522017C2 RU 2011152808/06 A RU2011152808/06 A RU 2011152808/06A RU 2011152808 A RU2011152808 A RU 2011152808A RU 2522017 C2 RU2522017 C2 RU 2522017C2
- Authority
- RU
- Russia
- Prior art keywords
- panel
- thrust reverser
- nacelle
- casing
- movable
- Prior art date
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/60—Control system actuates means
- F05D2270/66—Mechanical actuators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18568—Reciprocating or oscillating to or from alternating rotary
- Y10T74/18576—Reciprocating or oscillating to or from alternating rotary including screw and nut
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0902807A FR2946696B1 (fr) | 2009-06-10 | 2009-06-10 | Dispositif d'inversion de poussee |
FR09/02807 | 2009-06-10 | ||
PCT/FR2010/050953 WO2010142881A1 (fr) | 2009-06-10 | 2010-05-18 | Dispositif d'inversion de poussée |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2011152808A RU2011152808A (ru) | 2013-07-20 |
RU2522017C2 true RU2522017C2 (ru) | 2014-07-10 |
Family
ID=41600745
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2011152808/06A RU2522017C2 (ru) | 2009-06-10 | 2010-05-18 | Реверсор тяги |
Country Status (9)
Country | Link |
---|---|
US (1) | US9206765B2 (de) |
EP (1) | EP2440768B1 (de) |
CN (1) | CN102459856B (de) |
BR (1) | BRPI1013147A2 (de) |
CA (1) | CA2764437A1 (de) |
ES (1) | ES2406159T3 (de) |
FR (1) | FR2946696B1 (de) |
RU (1) | RU2522017C2 (de) |
WO (1) | WO2010142881A1 (de) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2726022C2 (ru) * | 2016-02-04 | 2020-07-08 | Сафран Эркрафт Энджинз | Силовая установка летательного аппарата |
RU2766970C2 (ru) * | 2017-08-07 | 2022-03-16 | Сафран Насель | Решетка реверсора тяги для гондолы летательного аппарата |
RU2808188C1 (ru) * | 2019-09-05 | 2023-11-24 | Сафран Насель | Реверсор тяги, содержащий тросовую кинематическую схему для ковшовых створок |
US11959439B2 (en) | 2019-09-05 | 2024-04-16 | Safran Nacelles | Thrust reverser provided with cable kinematics for scoop flaps |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2922058B1 (fr) * | 2007-10-04 | 2009-12-04 | Aircelle Sa | Actionneur lineaire telescopique pour deplacer un premier et un second elements relativement a un element fixe |
FR2922059B1 (fr) * | 2007-10-04 | 2014-07-04 | Aircelle Sa | Actionneur lineaire telescopique double action a systeme d'entrainement a moteur unique |
FR2994586B1 (fr) * | 2012-08-20 | 2014-08-08 | Aircelle Sa | Ensemble de poussee a grilles pour turboreacteur d'aeronef |
FR2996602B1 (fr) * | 2012-10-08 | 2018-04-06 | Sagem Defense Securite | Dispositif d'actionnement incluant un dispositif de verrouillage primaire |
US9573695B2 (en) | 2013-02-22 | 2017-02-21 | United Technologies Corporation | Integrated nozzle and plug |
US9631578B2 (en) | 2013-02-22 | 2017-04-25 | United Technologies Corporation | Pivot thrust reverser surrounding inner surface of bypass duct |
US20160025038A1 (en) * | 2013-03-15 | 2016-01-28 | United Technologies Corporation | Pivot door thrust reverser |
FR3007800B1 (fr) * | 2013-07-01 | 2017-10-20 | Aircelle Sa | Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles partiellement integrees dans les capots |
FR3009584B1 (fr) * | 2013-08-07 | 2018-03-30 | Safran Nacelles | Inverseur a volets integres |
FR3011820B1 (fr) * | 2013-10-11 | 2017-03-31 | Aircelle Sa | Nacelle pour moteur d'aeronef a tuyere de section variable |
FR3019857B1 (fr) * | 2014-04-11 | 2020-12-25 | Aircelle Sa | Inverseur de poussee de nacelle de turboreacteur comprenant une commande commune pour les capots mobiles et une tuyere variable |
US10077739B2 (en) * | 2014-04-24 | 2018-09-18 | Rohr, Inc. | Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle |
FR3021704B1 (fr) | 2014-05-30 | 2016-06-03 | Aircelle Sa | Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives |
US10309343B2 (en) | 2014-11-06 | 2019-06-04 | Rohr, Inc. | Split sleeve hidden door thrust reverser |
US10473057B2 (en) | 2015-12-14 | 2019-11-12 | Rohr, Inc. | Thrust reverser system with translating elements |
US9976696B2 (en) | 2016-06-21 | 2018-05-22 | Rohr, Inc. | Linear actuator with multi-degree of freedom mounting structure |
EP3282132B1 (de) * | 2016-08-08 | 2019-10-02 | Goodrich Actuation Systems Limited | Aktuator mit einer kupplung |
GB2564891A (en) * | 2017-07-26 | 2019-01-30 | Short Brothers Plc | Nacelle with thrust reverser |
US10975940B2 (en) * | 2017-08-24 | 2021-04-13 | Eaton Intelligent Power Limited | Actuator and method |
US10731738B2 (en) | 2017-11-27 | 2020-08-04 | Rohr, Inc. | Kinematic system with motion control device |
FR3077606B1 (fr) * | 2018-02-05 | 2020-01-17 | Airbus | Nacelle d'un turboreacteur comportant une porte exterieure d'inversion |
FR3078108B1 (fr) * | 2018-02-20 | 2020-01-31 | Safran Nacelles | Ensemble propulsif comportant des points de levage disposes sur des supports de verins d’inverseur de poussee |
US11358627B2 (en) * | 2019-11-06 | 2022-06-14 | Steering Solutions Ip Holding Corporation | System, method and apparatus for a telescopic lead screw for a steering column |
FR3105304B1 (fr) * | 2019-12-19 | 2021-12-10 | Safran Nacelles | Inverseur de poussée avec système d’actionnement anti-flambage |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3279182A (en) * | 1965-06-07 | 1966-10-18 | Gen Electric | Thrust reverser |
EP0851111A1 (de) * | 1996-12-26 | 1998-07-01 | Hispano-Suiza | Schubumkehrvorrichtung für ein Strahltriebwerk mit Klappe am Hinterteil |
RU2134812C1 (ru) * | 1996-02-15 | 1999-08-20 | Сосьете Испано-Сюиза | Устройство реверсирования тяги турбореактивного двигателя со створками, связанными с передней по потоку панелью |
EP1128052A1 (de) * | 2000-01-27 | 2001-08-29 | Hispano-Suiza Aérostructures | Schubumkehrvorrichtung mit beschaufeltem Gitter und festmontierter hinterer Struktur |
FR2887854A1 (fr) * | 2005-06-30 | 2007-01-05 | Airbus France Sas | Nacelle pour aeronef et aeronef muni d'au moins une telle nacelle |
FR2907512A1 (fr) * | 2006-10-23 | 2008-04-25 | Aircelle Sa | Inverseur de poussee a grilles pour moteur a reaction |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3302889A (en) * | 1964-10-01 | 1967-02-07 | United Aircraft Corp | Blow-in door ejector for stol |
US3601992A (en) * | 1970-06-10 | 1971-08-31 | Rohr Corp | Thrust reversing apparatus |
US3779010A (en) * | 1972-08-17 | 1973-12-18 | Gen Electric | Combined thrust reversing and throat varying mechanism for a gas turbine engine |
FR2683859B1 (fr) * | 1991-11-15 | 1994-02-18 | Hispano Suiza | Inverseur de poussee de turboreacteur a double flux. |
FR2754565B1 (fr) * | 1996-10-10 | 1999-01-08 | Hispano Suiza Sa | Inverseur de poussee a portes a debit de fuite controle |
FR2758161B1 (fr) * | 1997-01-09 | 1999-02-05 | Hispano Suiza Sa | Inverseur de poussee a grilles a installation de verin de commande optimisee |
CA2445934A1 (en) * | 2003-10-21 | 2005-04-21 | Propulsion Vectoring, L.P. | Jet engine nozzle with variable thrust vectoring and exhaust area |
US8127529B2 (en) * | 2007-03-29 | 2012-03-06 | United Technologies Corporation | Variable area fan nozzle and thrust reverser |
FR2917788B1 (fr) * | 2007-06-19 | 2009-07-24 | Aircelle Sa | Actionneur double action a effet programme |
FR2922058B1 (fr) * | 2007-10-04 | 2009-12-04 | Aircelle Sa | Actionneur lineaire telescopique pour deplacer un premier et un second elements relativement a un element fixe |
-
2009
- 2009-06-10 FR FR0902807A patent/FR2946696B1/fr not_active Expired - Fee Related
-
2010
- 2010-05-18 RU RU2011152808/06A patent/RU2522017C2/ru not_active IP Right Cessation
- 2010-05-18 CN CN201080025545.8A patent/CN102459856B/zh not_active Expired - Fee Related
- 2010-05-18 ES ES10728772T patent/ES2406159T3/es active Active
- 2010-05-18 WO PCT/FR2010/050953 patent/WO2010142881A1/fr active Application Filing
- 2010-05-18 EP EP10728772A patent/EP2440768B1/de active Active
- 2010-05-18 BR BRPI1013147A patent/BRPI1013147A2/pt not_active IP Right Cessation
- 2010-05-18 CA CA2764437A patent/CA2764437A1/fr not_active Abandoned
- 2010-05-18 US US13/321,831 patent/US9206765B2/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3279182A (en) * | 1965-06-07 | 1966-10-18 | Gen Electric | Thrust reverser |
RU2134812C1 (ru) * | 1996-02-15 | 1999-08-20 | Сосьете Испано-Сюиза | Устройство реверсирования тяги турбореактивного двигателя со створками, связанными с передней по потоку панелью |
EP0851111A1 (de) * | 1996-12-26 | 1998-07-01 | Hispano-Suiza | Schubumkehrvorrichtung für ein Strahltriebwerk mit Klappe am Hinterteil |
EP1128052A1 (de) * | 2000-01-27 | 2001-08-29 | Hispano-Suiza Aérostructures | Schubumkehrvorrichtung mit beschaufeltem Gitter und festmontierter hinterer Struktur |
FR2887854A1 (fr) * | 2005-06-30 | 2007-01-05 | Airbus France Sas | Nacelle pour aeronef et aeronef muni d'au moins une telle nacelle |
FR2907512A1 (fr) * | 2006-10-23 | 2008-04-25 | Aircelle Sa | Inverseur de poussee a grilles pour moteur a reaction |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2726022C2 (ru) * | 2016-02-04 | 2020-07-08 | Сафран Эркрафт Энджинз | Силовая установка летательного аппарата |
RU2766970C2 (ru) * | 2017-08-07 | 2022-03-16 | Сафран Насель | Решетка реверсора тяги для гондолы летательного аппарата |
RU2808188C1 (ru) * | 2019-09-05 | 2023-11-24 | Сафран Насель | Реверсор тяги, содержащий тросовую кинематическую схему для ковшовых створок |
US11959439B2 (en) | 2019-09-05 | 2024-04-16 | Safran Nacelles | Thrust reverser provided with cable kinematics for scoop flaps |
Also Published As
Publication number | Publication date |
---|---|
FR2946696B1 (fr) | 2012-04-20 |
US9206765B2 (en) | 2015-12-08 |
EP2440768B1 (de) | 2013-02-13 |
CN102459856B (zh) | 2014-04-16 |
ES2406159T3 (es) | 2013-06-05 |
FR2946696A1 (fr) | 2010-12-17 |
WO2010142881A1 (fr) | 2010-12-16 |
CN102459856A (zh) | 2012-05-16 |
BRPI1013147A2 (pt) | 2016-04-05 |
RU2011152808A (ru) | 2013-07-20 |
US20120067975A1 (en) | 2012-03-22 |
EP2440768A1 (de) | 2012-04-18 |
CA2764437A1 (fr) | 2010-12-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2522017C2 (ru) | Реверсор тяги | |
RU2538348C2 (ru) | Устройство реверса тяги | |
RU2499904C2 (ru) | Гондола двухконтурного турбореактивного двигателя | |
RU2538142C2 (ru) | Реверсор тяги | |
RU2529282C2 (ru) | Реверсор тяги гондолы двухконтурного турбореактивного двигателя и гондола двухконтурного турбореактивного двигателя, содержащая такой реверсор тяги | |
RU2470205C2 (ru) | Линейный телескопический исполнительный механизм для перемещения первого и второго элементов относительно неподвижного элемента | |
US10995700B2 (en) | Jet engine comprising a nacelle equipped with reverser flaps | |
US6065285A (en) | Thrust reverser for turbojet engine having scoop-forming doors cooperating with movable flow deflecting baffles | |
RU2570791C2 (ru) | Устройство для приведения в действие реверсора тяги с регулируемым соплом для гондолы турбореактивного двигателя и гондола, содержащая такое устройство | |
US9458793B2 (en) | Thrust reverser for an aircraft jet engine | |
EP0809011A2 (de) | Schubvectorsteuerung für Bläsertriebwerke | |
RU2577741C2 (ru) | Гондола для двухконтурного турбореактивного двигателя летательного аппарата | |
US9410500B2 (en) | Movable cascade turbojet thrust reverser having translatable reverser cowl causing variation in jet nozzle | |
RU2140558C1 (ru) | Устройство реверсирования тяги двухконтурного турбореактивного двигателя с отклоняющими поток препятствиями, связанными с первичным кожухом | |
US6145301A (en) | Thrust reverser for fan type turbojet engines using independently actuated pivoted thrust deflectors | |
US5284015A (en) | Turbojet engine thrust reverser with directional control | |
US20140245743A1 (en) | Double-acting linear actuator | |
US6076347A (en) | Turbojet engine thrust reverser having scoop doors and movable upstream visors | |
US10669971B2 (en) | Thrust reverser for a turbojet engine nacelle, comprising cascades partially integrated in the cowls | |
US20130228635A1 (en) | Turbojet engine nacelle | |
CN113071685A (zh) | 包括具有用于封闭旁通管道的罩系统的涡轮风扇发动机 | |
US20160273489A1 (en) | Fixed structure of a thrust reverser device | |
CN113071686A (zh) | 包括具有用于封闭旁通管道的罩系统的涡轮风扇发动机 | |
RU2571705C2 (ru) | Реверсор тяги, гондола, содержащая такой реверсор тяги, и способ изменения поперечного сечения сопла, реализуемый с помощью такого реверсора тяги | |
RU2139435C1 (ru) | Устройство реверсирования тяги турбореактивного двигателя со створками, связанными с передней по потоку панелью |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20160519 |